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Spacecraft self-contamination due to back-scattering of outgas productsThe back-scattering of outgas contamination near an orbiting spacecraft due to intermolecular collisions was analyzed. Analytical tools were developed for making reasonably accurate quantitative estimates of the outgas contamination return flux, given a knowledge of the pertinent spacecraft and orbit conditions. Two basic collision mechanisms were considered: (1) collisions involving only outgas molecules (self-scattering) and (2) collisions between outgas molecules and molecules in the ambient atmosphere (ambient-scattering). For simplicity, the geometry was idealized to a uniformly outgassing sphere and to a disk oriented normal to the freestream. The method of solution involved an integration of an approximation of the Boltzmann kinetic equation known as the BGK (or Krook) model equation. Results were obtained in the form of simple equations relating outgas return flux to spacecraft and orbit parameters. Results were compared with previous analyses based on more simplistic models of the collision processes.
Document ID
19760011126
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Robertson, S. J.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1976
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
LMSC-HREC-TR-D496676
NASA-CR-144197
Report Number: LMSC-HREC-TR-D496676
Report Number: NASA-CR-144197
Accession Number
76N18214
Funding Number(s)
CONTRACT_GRANT: NAS8-31440
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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